Modal decomposition of the unsteady non-reactive flow field in a swirl-stabilized combustor operated by a Lean Premixed injection system
Autor: | Salvador, F.J., Carreres, M., García-Tíscar, J., Belmar-Gil, M. |
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Zdroj: | In Aerospace Science and Technology May 2021 112 |
Databáze: | ScienceDirect |
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